The article was produced as a result of my internship at the Walter Bassett aerodynamics laboratory , where I was under the supervision of Prof. Ivan Marusic and PhD student Jason Ruan in the project "Active Control of Large-scale Structures in High Reynolds Number Turbulent Boundary Layers".

The article reviews three methods implemented in the laboratory to measure skin friction.

1. Hot-wire anemometry
2. Hot-film anemometry
3. Particle Image Velocimetry (PIV)

We carried out all the experiments in the High Reynolds Number Boundary Layer Wind Tunnel. To analyse the results, I acquired basic skills in signal post-processing.

• Publication PDFInternational Journal of Engineering and Technology IJET - ENGG Journals
• CitationCristian Rendon-Cardona, Zhoushun Ruan, Oscar Ruiz-Salguero. International Journal of Engineering and Technology, e-ISSN : 0975-4024 p-ISSN : 2319-8613, volume 12, issue 1, Publisher Eng Journals. url= http://www.enggjournals.com/ijet/abstract.html?file=20-12-01-002, doi= DOI : 10.21817/ijet/2020/v12i1/201201002 Published: 29 February 2020